EP2653588A2 - Matériau pour composant résistant à la chaleur - Google Patents

Matériau pour composant résistant à la chaleur Download PDF

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Publication number
EP2653588A2
EP2653588A2 EP13020053.8A EP13020053A EP2653588A2 EP 2653588 A2 EP2653588 A2 EP 2653588A2 EP 13020053 A EP13020053 A EP 13020053A EP 2653588 A2 EP2653588 A2 EP 2653588A2
Authority
EP
European Patent Office
Prior art keywords
less
coating
based superalloy
heat resistant
layer
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
EP13020053.8A
Other languages
German (de)
English (en)
Other versions
EP2653588A3 (fr
Inventor
Hiroshi Harada
Akihiro Sato
Kyoko Kawagishi
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
National Institute for Materials Science
Original Assignee
National Institute for Materials Science
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
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First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=37053394&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=EP2653588(A2) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by National Institute for Materials Science filed Critical National Institute for Materials Science
Publication of EP2653588A2 publication Critical patent/EP2653588A2/fr
Publication of EP2653588A3 publication Critical patent/EP2653588A3/fr
Withdrawn legal-status Critical Current

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Classifications

    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C30/00Coating with metallic material characterised only by the composition of the metallic material, i.e. not characterised by the coating process
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00Layered products comprising a layer of metal
    • B32B15/01Layered products comprising a layer of metal all layers being exclusively metallic
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C19/00Alloys based on nickel or cobalt
    • C22C19/03Alloys based on nickel or cobalt based on nickel
    • C22C19/05Alloys based on nickel or cobalt based on nickel with chromium
    • C22C19/051Alloys based on nickel or cobalt based on nickel with chromium and Mo or W
    • C22C19/057Alloys based on nickel or cobalt based on nickel with chromium and Mo or W with the maximum Cr content being less 10%
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C19/00Alloys based on nickel or cobalt
    • C22C19/03Alloys based on nickel or cobalt based on nickel
    • C22C19/05Alloys based on nickel or cobalt based on nickel with chromium
    • C22C19/058Alloys based on nickel or cobalt based on nickel with chromium without Mo and W
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C28/00Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
    • C23C28/02Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D only coatings only including layers of metallic material
    • C23C28/021Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D only coatings only including layers of metallic material including at least one metal alloy layer
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C28/00Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
    • C23C28/02Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D only coatings only including layers of metallic material
    • C23C28/028Including graded layers in composition or in physical properties, e.g. density, porosity, grain size
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12493Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12771Transition metal-base component
    • Y10T428/12861Group VIII or IB metal-base component
    • Y10T428/12944Ni-base component

Definitions

  • a diffusion barrier coating For the purpose of preventing the diffusion of elements through the substrate /coating interface, a diffusion barrier coating is examined (for example, see Patent Document 1).
  • the diffusion barrier coating has a multilayer, structure to complicate the coating process, and, in addition, since a substrate and a coating material are not in the thermodynamical equilibrium state, there is some limit of the effect as a natural result.
  • the invention is nineteenthly characterized in that an alloy layer having a composition containing Al: not less than 6.1 wt% to not more than 10.6 wt%, Ta: not less than 0 wt% to not more than 10.5 wt%, Mo: not less than 0 wt% to not more than 3.9 wt%, W: not less than 0 wt% to not more than 8.2 wt%, Re: not less than 0 wt% to not more than 3.4 wt%, Ti: not less than 0 wt% to not more than 1.7 wt%, Hf: not less than 0 wt% to not more than 1.15 wt%, Cr: not less than 0.4 wt% to not more than 4.0 wt%, Co: not less than 3.2 wt% to not more than 10.2 wt%, Ru: not less than 0 wt% to not more than 6.2 wt%, Nb: not less than 0 wt% to not more
  • the Ni-based superalloys having a predetermined composition range to be a substrate are a single crystal alloy further excellent in creep property, and the alloy to be coated is an alloy that exhibits thermodynamic equilibrium with the Ni-based superalloy and is, at the same time, excellent in oxidation resistance, therefore a heat resistant material excellent in high-temperature durability can be obtained.
  • Fig. 6 the result of a 1100°C ⁇ 1 H cycle oxidation test on a sample obtained in Example 2 is shown while comparing with an Ni-based superalloy used for a substrate. It can be said that the sample obtained in Example 2 exhibits excellent oxidation resistance as compared with the substrate, satisfies both the oxidation resistance and stability, and is a heat resistant material having a remarkably excellent high-temperature durability.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Other Surface Treatments For Metallic Materials (AREA)
  • Coating By Spraying Or Casting (AREA)
  • Laminated Bodies (AREA)
EP13020053.8A 2005-03-28 2006-03-28 Matériau pour composant résistant à la chaleur Withdrawn EP2653588A3 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
JP2005092542 2005-03-28
EP06730216.6A EP1876263B1 (fr) 2005-03-28 2006-03-28 Element resistant a la chaleur

Related Parent Applications (2)

Application Number Title Priority Date Filing Date
EP06730216.6 Division 2006-03-28
EP06730216.6A Division-Into EP1876263B1 (fr) 2005-03-28 2006-03-28 Element resistant a la chaleur

Publications (2)

Publication Number Publication Date
EP2653588A2 true EP2653588A2 (fr) 2013-10-23
EP2653588A3 EP2653588A3 (fr) 2013-11-13

Family

ID=37053394

Family Applications (2)

Application Number Title Priority Date Filing Date
EP06730216.6A Expired - Fee Related EP1876263B1 (fr) 2005-03-28 2006-03-28 Element resistant a la chaleur
EP13020053.8A Withdrawn EP2653588A3 (fr) 2005-03-28 2006-03-28 Matériau pour composant résistant à la chaleur

Family Applications Before (1)

Application Number Title Priority Date Filing Date
EP06730216.6A Expired - Fee Related EP1876263B1 (fr) 2005-03-28 2006-03-28 Element resistant a la chaleur

Country Status (5)

Country Link
US (1) US8221901B2 (fr)
EP (2) EP1876263B1 (fr)
JP (1) JP4845140B2 (fr)
CN (1) CN101146931B (fr)
WO (1) WO2006104138A1 (fr)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP5334017B2 (ja) * 2006-09-13 2013-11-06 独立行政法人物質・材料研究機構 耐熱部材
US20120070303A1 (en) * 2009-08-10 2012-03-22 Yasuhiro Aoki Ni-BASED SINGLE CRYSTAL SUPERALLOY AND TURBINE BLADE
EP2550374A1 (fr) 2010-03-23 2013-01-30 Siemens Aktiengesellschaft Couche d'accrochage ou alliage métallique ayant une température de transition / ' élevée et un composant
US20110256421A1 (en) * 2010-04-16 2011-10-20 United Technologies Corporation Metallic coating for single crystal alloys
JP5660428B2 (ja) 2010-04-20 2015-01-28 独立行政法人物質・材料研究機構 耐熱コーティング材
EP2631324A4 (fr) * 2010-10-19 2014-04-16 Nat Inst For Materials Science Élément en un superalliage à base de ni contenant une couche d'accrochage résistante à la chaleur
US20160214350A1 (en) 2012-08-20 2016-07-28 Pratt & Whitney Canada Corp. Oxidation-Resistant Coated Superalloy
JPWO2015020007A1 (ja) * 2013-08-05 2017-03-02 国立研究開発法人物質・材料研究機構 酸化物粒子分散強化型Ni基超合金
CN105088018A (zh) * 2015-09-10 2015-11-25 钢铁研究总院 一种高强度、抗氧化的钴基高温合金
CN105463257B (zh) * 2015-12-08 2018-04-24 南通金源智能技术有限公司 一种镍基高温合金粉
CN106756252B (zh) * 2016-12-29 2019-03-22 沈阳大陆激光工程技术有限公司 一种用于重型燃机轮毂榫齿修复的镍基合金粉末
CN108796308B (zh) * 2017-05-04 2020-09-18 中国科学院金属研究所 一种裂纹敏感性低、低密度、高强度镍基高温合金
FR3072717B1 (fr) * 2017-10-20 2019-10-11 Safran Piece de turbine en superalliage comprenant du rhenium et procede de fabrication associe
WO2021052704A1 (fr) * 2019-09-19 2021-03-25 Basf Se Revêtements protecteurs à haute température, en particulier destinés à être utilisés dans des processus pétrochimiques
CN111139377B (zh) * 2020-02-10 2021-03-26 中国科学院金属研究所 一种高温合金及其制备方法
EP4289613A1 (fr) 2022-06-12 2023-12-13 Pratt & Whitney Canada Corp. Revêtements résistants à l'oxydation et au srz sur les superalliages de nickel
CN116287873B (zh) * 2023-05-19 2023-08-04 北京煜鼎增材制造研究院股份有限公司 一种1100℃用镍基高温合金及其增材制造方法

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20040229075A1 (en) 2003-05-16 2004-11-18 Brian Gleeson High-temperature coatings with Pt metal modified gamma-Ni + gamma'-Ni3Al alloy compositions
US6830827B2 (en) 2000-03-07 2004-12-14 Ebara Corporation Alloy coating, method for forming the same, and member for high temperature apparatuses

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DE3683091D1 (de) * 1985-05-09 1992-02-06 United Technologies Corp Schutzschichten fuer superlegierungen, gut angepasst an die substrate.
US4758480A (en) * 1987-12-22 1988-07-19 United Technologies Corporation Substrate tailored coatings
DE69732046T2 (de) 1997-10-30 2005-12-08 Alstom Schutzbeschichtung für hochtemperatur
US6190471B1 (en) * 1999-05-26 2001-02-20 General Electric Company Fabrication of superalloy articles having hafnium- or zirconium-enriched protective layer
JP3577252B2 (ja) * 2000-01-31 2004-10-13 新日軽株式会社 片開き親子方式の伸縮門扉
JP3840555B2 (ja) * 2001-05-30 2006-11-01 独立行政法人物質・材料研究機構 Ni基単結晶超合金
JP3916484B2 (ja) * 2002-03-05 2007-05-16 独立行政法人科学技術振興機構 耐高温酸化性に優れたNi合金耐熱材料およびその製造方法
US6919042B2 (en) * 2002-05-07 2005-07-19 United Technologies Corporation Oxidation and fatigue resistant metallic coating
US7288328B2 (en) * 2004-10-29 2007-10-30 General Electric Company Superalloy article having a gamma-prime nickel aluminide coating
JP5344453B2 (ja) * 2005-09-27 2013-11-20 独立行政法人物質・材料研究機構 耐酸化性に優れたNi基超合金
JP5334017B2 (ja) * 2006-09-13 2013-11-06 独立行政法人物質・材料研究機構 耐熱部材

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6830827B2 (en) 2000-03-07 2004-12-14 Ebara Corporation Alloy coating, method for forming the same, and member for high temperature apparatuses
US20040229075A1 (en) 2003-05-16 2004-11-18 Brian Gleeson High-temperature coatings with Pt metal modified gamma-Ni + gamma'-Ni3Al alloy compositions

Also Published As

Publication number Publication date
CN101146931B (zh) 2010-06-23
JP4845140B2 (ja) 2011-12-28
CN101146931A (zh) 2008-03-19
EP2653588A3 (fr) 2013-11-13
JPWO2006104138A1 (ja) 2008-09-11
EP1876263B1 (fr) 2014-05-14
WO2006104138A1 (fr) 2006-10-05
EP1876263A4 (fr) 2010-12-22
US20080226937A1 (en) 2008-09-18
EP1876263A1 (fr) 2008-01-09
US8221901B2 (en) 2012-07-17

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